SEP Transfers in the Earth-Moon System
•Three Power levels:80kW,100kW and 200kW
•Five Specific Impulse Values: 2000s, 3000s, 4000s, 5000s, 10000s
Payload Mass obtained with a preliminary mass breakdown:
* Solar arrays: 20 kg/kW * PPUs and thrusters: 3 kg/kW * Tanks and related structures: 20% of propellant mass
Brian Wang is a Futurist Thought Leader and a popular Science blogger with 1 million readers per month. His blog Nextbigfuture.com is ranked #1 Science News Blog. It covers many disruptive technology and trends including Space, Robotics, Artificial Intelligence, Medicine, Anti-aging Biotechnology, and Nanotechnology.
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